[IGSREPORT-29185] Wk 2247 IGLOS Final Orbits
acc
acc at igs.org
Fri Feb 17 06:26:43 UTC 2023
Author: AC Coordinator / GA MIT
sum-file Version 2.0
IGLOS Orbit Combination - Week 2247 (Jan 29, 2023 - Feb 04, 2023)
Contact: acc at igs.org
COMBINATION STRATEGY:
---------------------
Ephemeris are combined as weighted averages computed over all centres.
Each centre and satellite is given a position weight computed from the
center's absolute deviation to the unweighted average orbit after removing
small differences in the reference frames. These weights were applied in a
second iteration to estimate Helmert transformation parameters for each
center. Finally the transformation parameters with respect to the combined
solution and the RMS of the fit are reported in Tables 2.2247.
For long arc computations the Earth Orientation Parameters (EOPs) are fixed
to the values of the final IGS (GPS) combination.
SOFTWARE:
---------
The weighted average software used was originally developed by T. Springer
and G. Beutler in 1993. The GPS long arc orbit analysis software used here for
individual centre ephemeris evaluation was developed by Beutler et al. at the
Astronomical Institute of the University of Bern (AIUB). For more details on
the orbit combination and complete references for both software see:
Beutler G., Kouba J. and T. Springer, 1995, Combining the orbits of the IGS
Analysis Centers, Bulletin Geodesique, 69, pp 200-222.
Kouba J., Mireault Y. and F. Lahaye, 1995, 1994 IGS Orbit/Clock Combination
and Evaluation, Appendix I of the Analysis Coordinator Report, International
GPS Service for Geodynamics (IGS) 1994 Annual Report, pp. 70-94.
Kouba J. and Y. Mireault, 1996, IGS Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1995 Annual Report,
pp. 45-76.
Kouba J. and Y. Mireault, 1997, Analysis Coordinator Report,
International GPS Service for Geodynamics (IGS) 1996 Annual Report,
pp. 55-100.
Weber R., 2000, IGS Technical Report 1999
PRODUCTS GENERATED:
-------------------
The combined IGL-ephemerides are written to daily files in the SP3-format.
The satellite accuracy codes in the header are based on the weighted rms.
for each satellite. Note, that the result files contain all satellites
that were analysed by at least one center. We refer to the 'REMARKS' section
below, in case a satellite or center was excluded from the combination.
The following naming convention is used for the result files:
igl2247[0-6].sp3 IGLOS-PP Glonass ephemerides files for days 0-6
of GPS Week 2247 in the SP3 format.
igl22477.sum Combination Report for GPS Week 2247.
REMARKS concerning the IGL Orbit Combination:
---------------------------------------------
Starting 16-Sep-2012 (GPS Week 1706, day 0, MJD 56186) the CODE Analysis Center
began submitting two solutions: COD (3d SNX with 3d orbital arcs) and COF (1d
SNX with 1d orbital arcs). The COF clocks and orbits are included for
comparison only; the COD solution is included with weight.
Starting 28-Nov-2022 (GPS week 2238) the IGS Analysis Centers started submitting
repro3-standard multi-GNSS solutions in the IGS20 reference frame. These solutions
are used in the IGS combination of GLONASS orbits.
1. Broadcast (brd) orbits and clocks are included in the combination for
statistics only.
2. The iac orbits did not change to the IGS20/igs20.atx frame from GPS week 2238
until TBA, therefore the iac orbits are not used in the orbit combinations but
are inlcuded for statistics only from GPS week 2238 until TBA.
3. Having only a few satellites the mcc orbits are included in the combination
for statistics only. The grg orbits are introduced for the first time
starting 02-Jan-2011 (GPS Week 1617) but only for statistics until
22-May-2011 (GPS Week 1637). The bkg orbits were no longer included after
21-May 2011 (GPS Week 1636). The emx orbits are introduced with full weight
for the first time starting 11-Sep-2011 (GPS Week 1653).
4. From 01-May-2005 (GPS Week 1321; MJD 53491) [IGSMAIL-5151] until 4-Nov-2006
BKG, ESA, and CODE referred their GLONASS orbit products to the following
satellite antenna offset (SAO) values (expressed in the spacecraft body
frame):
X/Y/Z = 0.000/0.000/0.000 meter for GLONASS and
X/Y/Z = -0.545/0.000/0.000 meter for GLONASS-M SVs.
Starting 5-Nov-2006 (GPS Week 1400, day 0, MJD 54044) until 16-Apr-2011
(GPS Week 1631, day 6, MJD 55667) the absolute antenna model is introduced
(IGSMAIL #5438). The antenna phase center offsets and phase center variations
are given in the file:
https://files.igs.org/pub/station/general/igs05.atx
These antenna calibrations are also used in the homogeneously reprocessed IGS
products from GPS Weeks 730 to 1459 (1994-2007); see IGSMAIL #6136.
Starting 17-Apr-2011 (GPS Week 1632, day 0, MJD 55668) the absolute antenna
model is updated (IGSMAIL #6255 & #6374) as given in the file:
https://files.igs.org/pub/station/general/igs08.atx
Starting 29-Jan-2017 (GPS Week 1934, day 0, MJD 57782) the absolute antenna
model file has been updated to igs14.atx to be consistent with IGS14.
See IGSMAIL #7399 for more information
https://files.igs.org/pub/station/general/igs14.atx
5. The satellite clock values in the combined orbit files are taken from the
broadcast files. The following gps/glonass time offsets were added to the
broadcast clocks. Before GPS Week 1637, the time offsets were derived
from the bkg summary files; starting Week 1637 the offsets are derived
from the gfz summary files.
Day | applied clock offset
----+---------------------
0 | 1.0 ns
1 | -1.9 ns
2 | -13.4 ns
3 | -0.7 ns
4 | 0.2 ns
5 | 0.0 ns
6 | -0.8 ns
6. The following orbit solutions were excluded from the combination
because they were biasing the weighted average (generally indicated
by long arc RMS).
Day | Centre | PRN list
----+--------+---------------
0 | ESA | R22
1 | ESA | R20 R22
2 | ESA | R20 R22
3 | ESA | R20 R22
4 | ESA | R22
5 | ESA | R20 R22
6 | ESA | R22
ORBIT COMBINATION AND EVALUATION STATISTICS:
--------------------------------------------
Table 1 summarizes all statistics for the week. It contains means and standard
deviations over the week of satellite ephemeris and clock correction
transformation parameters for each centre (Tables 1.2247, 1a.2247).
Table 2 contains the complete ephemeris and clock correction transformation
parameters (includes both the apriori and a posteriori values) for each
centre and each day (Tables 2.2247.0-6)
Table 3 contains two types of daily RMS for each satellite and centre, along
with the computed satellite position sigmas for the combined orbits
(tables 3.2247.0-6).
The first type of satellite RMS is based on orbit combination and the
second RMS type is a result of the 7-day arc evaluation of each centre
ephemerides.
Table 1: Week 2247 summary. (Jan 29, 2023 - Feb 04, 2023)
Table 1.2247.a GPS week : 2247 MJD: 59973.0-59979.0
Mean and standard deviations of transformation parameters to the
combined IGL orbit.
WRMS - orbit RMS weighted by the SP3 header accuracy codes.
STA - Mean number of stations in the daily solutions.
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 5 -2 1 37 .05 19 16 | 37733 -732 2995 8169
| 0 0 1 15 13 28 .03 | 5278 2179
esa n/a| 0 0 -3 -27 3 -21 -.25 44 30 | -2621 -757 2998 8323
| 1 0 1 17 13 20 .06 | 4888 2078
gfz n/a| 0 2 0 39 2 -12 -.13 28 20 | 0 -544 2997 8024
| 0 1 2 10 15 18 .06 | 0 1897
grg n/a| 1 -2 -3 -17 -12 -17 .24 22 17 | -2036 -625 2990 7392
| 1 1 2 17 16 50 .02 | 5016 1812
iac n/a| -1 0 -4 1 33 -48 -.27 24 20 | -340 -7 2987 8595
| 1 1 4 22 24 88 .10 | 5224 696
Table 1.2247.b GPS week : 2247 MJD: 59973.0-59979.0
Satellite position sigmas for the combined orbits
(coded in the IGS SP3 orbit files).
"E" flags eclipsing satellites.
Units: mm.
Day of GPS week
PRN | 0 1 2 3 4 5 6 | Remarks
------+------------------------------------+------------------------------------------
R01 | 20 21 20 24 20 18 31 |
R02 | 7 7 8 7 7 8 7 |
R03 | 9 8 6 7 10 8 9 |
R04 | 9 8 8 7 8 8 8 |
R05 | 7 9 10 6 10 7 7 |
R07 | 9 9 8 9 7 8 9 |
R08 | 11 9 8 7 8 9 11 |
R09 | 6 8 7 7 8 6 10 |
R11 | 7 7 7 10 10 7 6 |
R12 | 9 12 9 10 6 8 9 |
R13 | 20 17 17 17 26 19 19 |
R14 | 6 6 7 8 6 7 6 |
R15 | 7 9 8 10 7 7 8 |
R16 | 26 24 26 22 24 20 21 |
R17 | 9 11 8 7 8 10 9 |
R18 | 8 8 10 10 9 7 9 |
R19 | 25 22 19 30 27 26 22 |
R20 | 47 31 23 20 41 44 47 |
R21 | 8 11 9 8 9 12 9 |
R22 | 7 12 12 8 12 9 12 |
R24 | 11 12 13 10 13 12 12 |
Table 1.2247.c GPS week : 2247 MJD: 59973.0-59979.0
Daily transformation of broadcast orbits (brd) to the combined IGL orbit.
Mean and standard deviations of the transformation parameters for the
whole gpsweek.
CEN WEEK DAY | DX DY DZ RX RY RZ SCL RMS WRMS | TOFT TDRFT
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm] | [ps] [ps/d]
-------------+------------------------------------------------------------+----------------
brd 2247 0 | 45 57 105 -427 -191 -1105 79.4 1135 1135 | 1030 0
brd 2247 1 | -45 -9 128 -1064 -2591 -8530 79.7 1476 1476 | -1949 0
brd 2247 2 | 50 41 82 -919 -679 -1201 81.2 1468 1468 | -13443 0
brd 2247 3 | 0 45 136 -1512 2143 2557 80.1 1502 1502 | -682 0
brd 2247 4 | 29 -54 88 -285 935 1524 78.7 1765 1765 | 184 0
brd 2247 5 | 108 -3 71 189 2174 -1925 78.8 1338 1338 | 1 0
brd 2247 6 | -52 -73 65 1383 1408 -3281 79.7 1301 1301 | -830 0
-------------+------------------------------------------------------------+----------------
brd 2247 mean| 19 0 96 -376 457 -1708 79.7 1426 1426 | -2241 0
brd 2247 sdev| 56 51 27 956 1728 3612 .9 197 197 | 5026 0
Table 2: Daily transformation of each centre to the combined IGL orbit and
clocks for each day of the week. The transformation displayed is the
sum of a priori and estimated transformations.
WRMS - RMS weighted by the centres SP3 header accuracy codes.
STA - Number of stations in the daily solutions.
Table 2.2247.0 GPS week: 2247 Day: 0 MJD: 59973
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 4 -8 -17 -1 .05 23 18 | 42069 2828 2796 7607
esa n/a| 0 1 -2 4 5 -8 -.23 37 21 | -516 2695 2820 6675
gfz n/a| 0 1 0 49 20 -31 -.14 30 15 | 0 2533 2817 7421
grg n/a| 1 0 -2 -26 0 46 .21 23 16 | -378 2258 2795 6994
iac n/a| -2 0 2 -27 55 -96 -.36 24 20 | 2273 1158 2810 8026
Table 2.2247.1 GPS week: 2247 Day: 1 MJD: 59974
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 3 15 21 70 .06 17 16 | 42330 -4161 2657 7503
esa n/a| -1 0 -1 -31 18 -3 -.17 46 25 | -3006 -3739 2648 6446
gfz n/a| -1 2 -2 45 -10 -23 -.10 26 25 | 0 -3596 2653 7364
grg n/a| 3 -3 -2 -52 -13 -59 .24 24 21 | -148 -3511 2661 6686
iac n/a| 1 0 -3 21 63 140 -.36 23 20 | 584 -607 2645 7937
Table 2.2247.2 GPS week: 2247 Day: 2 MJD: 59975
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 2 -30 15 39 .01 17 15 | 26534 -179 2993 8653
esa n/a| -2 0 -5 -30 17 -17 -.18 43 28 | -11576 -724 3020 7575
gfz n/a| 0 2 0 50 -10 19 -.08 23 18 | 0 -817 3021 8483
grg n/a| 1 -2 0 -1 -47 -100 .24 21 18 | -13405 -319 3003 7789
iac n/a| -3 0 -7 6 7 -62 -.15 24 20 | -12095 569 3009 9126
Table 2.2247.3 GPS week: 2247 Day: 3 MJD: 59976
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 7 0 0 76 .05 20 19 | 38238 -932 2695 7210
esa n/a| -1 -1 -1 -40 -5 -36 -.29 48 30 | -5348 -1152 2727 10310
gfz n/a| 0 0 -2 34 0 -8 -.12 24 15 | 0 -920 2724 7145
grg n/a| 1 -1 -3 -8 -13 -35 .25 18 15 | -363 -888 2713 6520
iac n/a| 0 0 -2 -21 32 -78 -.19 24 19 | 1062 182 2711 7733
Table 2.2247.4 GPS week: 2247 Day: 4 MJD: 59977
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 1 6 10 -12 8 .04 17 16 | 38796 -570 3226 9190
esa n/a| 0 0 -2 -51 4 -3 -.27 45 35 | -1336 166 3182 8241
gfz n/a| -1 4 0 32 24 -33 -.08 29 23 | 0 103 3205 9000
grg n/a| 2 -4 -6 -15 -11 9 .21 22 16 | 167 -145 3200 8392
iac n/a| -2 0 -6 15 29 -84 -.33 24 19 | 2486 -509 3196 9594
Table 2.2247.5 GPS week: 2247 Day: 5 MJD: 59978
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| 0 0 5 3 6 33 .09 18 15 | 37752 264 3474 8289
esa n/a| 0 0 -1 -16 -19 -59 -.35 48 39 | 4157 63 3452 7553
gfz n/a| 0 2 3 44 -12 -2 -.21 31 19 | 0 485 3444 8140
grg n/a| 0 -3 -7 -11 0 18 .25 20 14 | -129 239 3413 7431
iac n/a| 0 0 -10 -10 -2 -28 -.13 24 21 | 1746 -86 3427 8636
Table 2.2247.6 GPS week: 2247 Day: 6 MJD: 59979
CENT STA| DX DY DZ RX RY RZ SCL RMS WRMS| TOFT TDRFT SDEV RMS
| [mm] [mm] [mm] [uas] [uas] [uas] [ppb] [mm] [mm]| [ps] [ps/d] [ps] [ps]
--------+----------------------------------------------------+------------------------------
cod n/a| -1 0 6 -11 0 38 .01 22 16 | 38415 -2375 3129 8732
esa n/a| 1 0 -6 -30 2 -23 -.25 40 30 | -725 -2612 3137 11463
gfz n/a| 0 4 2 22 5 -7 -.21 30 23 | 0 -1601 3117 8619
grg n/a| 1 -3 -4 -5 1 -1 .26 25 19 | 3 -2013 3151 7937
iac n/a| -1 1 -4 29 46 -130 -.34 24 22 | 1559 -761 3113 9118
Table 3: Daily fit for each satellite and each centre resulting from weighted
average combination and from long arc orbit dynamics (7-day). The
first IGL column gives resulting satellite accuracy measures found in
SP3 header. The last IGL column gives the RMS fit of the IGL orbit
when processed through the 7-day arc evaluation.
"E" stands for eclipsing satellites (earth).
"M" stands for eclipsing satellites (moon).
"X" stands for excluded from the statistics but included in IGL orbit.
"T" stands for Total long arc orbit RMS for all satellites.
"NE" stands for long arc orbit RMS for Non-Eclipsing satellites only.
"MEDI" stands for median of the centre's satellite RMS.
"MD"
Units: mm.
Table 3.2247.0 GPS week: 2247 Day: 0 MJD: 59973
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 758 31 48 42 17 48 20 | 75 63 93 66 78 68
R02E | 845 9 13 15 11 20 7 | 42 44 36 48 34 41
R03E | 559 15 10 13 18 9 8 | 74 72 70 82 76 75
R04E | 2080 16 17 11 14 20 8 | 44 40 42 46 43 41
R05E | 1455 12 13 14 10 15 7 | 70 67 70 74 68 70
R07E | 848 14 17 18 8 23 8 | 54 50 56 57 48 53
R08E | 718 17 25 16 16 17 10 | 60 67 59 64 62 61
R09 | 666 11 13 7 11 18 6 | 29 35 31 36 32 31
R11 | 450 10 14 14 9 12 6 | 35 43 41 40 36 38
R12 | 991 12 9 19 18 19 9 | 41 41 49 34 46 39
R13 | 1403 25 39 34 37 23 19 | 53 55 59 58 49 54
R14 | 729 12 12 9 9 25 6 | 50 55 53 46 51 49
R15 | 637 17 14 8 9 12 7 | 57 50 51 52 49 52
R16 | 598 26 23 79 30 23 26 | 65 61 67 64 63 63
R17 | 660 7 22 17 10 18 8 | 66 52 71 75 69 66
R18 | 825 17 15 11 12 16 8 | 52 68 63 71 65 62
R19 | 2384 38 51 41 42 30 24 | 81 56 79 85 73 68
R20 | 1451 64 124 71 62 42 46 | 132 87 148 107 117 114
R21 | 438 16 21 7 12 17 8 | 86 58 79 78 78 76
XR22 | 2260 --- 337 8 6 24 7 | --- 155 44 51 48 46
R24 | 1575 16 31 14 15 26 11 | 79 53 75 84 79 73
------+------------------------------------+--------------------------------
RMS | 1135 23 37 30 23 24 |T 62 60 63 62 60 59
WRMS | 1135 18 21 15 16 20 |NE 63 62 65 62 61 59
MEDI | 825 16 17 14 12 20 |MD 57 55 59 64 62 61
Table 3.2247.1 GPS week: 2247 Day: 1 MJD: 59974
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1219 30 48 44 21 37 21 | 66 69 72 54 66 60
R02E | 1170 8 16 12 13 18 7 | 36 34 35 46 36 36
R03E | 764 13 18 13 14 17 8 | 92 100 102 99 90 97
R04E | 1963 12 21 11 10 16 8 | 44 40 46 47 42 43
R05E | 2159 13 13 19 17 25 9 | 54 52 61 59 68 55
R07E | 1901 9 17 16 16 14 8 | 54 44 49 52 53 48
R08E | 867 10 27 10 15 18 9 | 52 52 48 54 40 51
R09 | 826 15 20 8 12 20 8 | 22 20 15 21 27 15
R11 | 646 13 17 8 10 20 7 | 15 23 15 23 18 15
R12 | 1184 10 10 21 32 17 11 | 23 22 31 24 25 20
R13 | 1356 12 32 36 37 33 17 | 29 31 60 27 26 34
R14 | 820 7 12 11 12 16 6 | 25 30 32 23 26 25
R15 | 947 17 17 16 12 19 9 | 25 19 25 21 33 19
R16 | 786 28 30 66 23 27 23 | 35 27 30 25 39 28
R17 | 548 8 27 14 27 20 11 | 40 32 40 57 48 40
R18 | 727 15 16 8 16 15 8 | 29 38 32 45 37 33
R19 | 2821 33 54 23 43 24 22 | 52 30 34 62 41 41
R20 | 3346 28 173 53 47 42 30 | 58 70 83 80 71 74
R21 | 494 19 19 13 20 15 10 | 47 33 27 40 39 34
XR22 | 2145 --- 356 12 11 19 11 | --- 68 25 30 25 26
R24 | 679 9 36 11 25 18 12 | 40 29 48 61 48 43
------+------------------------------------+--------------------------------
RMS | 1475 17 46 26 24 23 |T 41 41 43 45 42 39
WRMS | 1475 16 25 25 21 20 |NE 33 33 35 38 35 31
MEDI | 947 13 20 13 16 19 |MD 40 33 35 46 39 36
Table 3.2247.2 GPS week: 2247 Day: 2 MJD: 59975
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 585 24 55 36 14 33 19 | 54 55 74 53 60 53
R02E | 486 9 17 14 14 21 7 | 46 45 40 56 46 45
R03E | 605 9 15 8 11 16 6 | 73 61 71 78 64 70
R04E | 910 11 14 13 17 17 8 | 53 56 55 56 60 53
R05E | 1741 12 18 19 16 17 9 | 52 55 52 58 53 52
R07E | 1911 11 13 12 17 19 7 | 52 59 55 56 46 53
R08E | 1414 13 17 11 13 24 7 | 40 44 40 49 43 41
R09 | 801 9 15 8 14 20 6 | 26 32 26 32 37 26
R11 | 575 11 13 8 15 22 7 | 28 34 28 36 36 29
R12 | 1513 12 11 12 24 23 9 | 23 24 26 24 34 21
R13 | 1162 32 25 26 31 18 16 | 39 28 34 38 42 29
R14 | 550 4 14 10 18 19 7 | 34 42 39 29 41 35
R15 | 604 15 10 11 18 20 8 | 40 37 40 33 37 36
R16 | 570 29 30 68 33 24 25 | 46 45 45 41 45 42
R17 | 589 7 21 9 19 18 8 | 44 37 38 57 38 42
R18 | 437 15 23 8 17 18 9 | 37 41 38 47 41 38
R19 | 2997 30 53 16 28 46 19 | 70 39 54 59 81 54
R20 | 2988 24 158 37 37 47 23 | 89 67 89 95 71 92
R21 | 548 7 26 18 6 15 9 | 62 47 73 68 58 63
XR22 | 2128 --- 361 10 13 22 11 | --- 104 32 39 45 32
R24 | 2874 16 30 11 28 11 12 | 54 37 49 65 46 49
------+------------------------------------+--------------------------------
RMS | 1467 17 43 23 21 24 |T 48 47 47 50 48 45
WRMS | 1467 15 28 18 18 20 |NE 45 43 43 47 46 42
MEDI | 801 12 18 12 17 20 |MD 46 44 40 53 45 42
Table 3.2247.3 GPS week: 2247 Day: 3 MJD: 59976
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 2308 32 70 40 19 38 23 | 53 59 77 44 47 46
R02E | 917 10 16 11 10 17 6 | 32 34 41 38 30 35
R03E | 630 13 12 11 13 10 7 | 90 84 84 92 85 87
R04E | 977 13 16 12 8 20 7 | 44 35 45 49 40 43
R05E | 1164 11 12 9 10 14 6 | 58 65 73 71 75 66
R07E | 815 14 18 17 11 15 8 | 59 65 58 63 56 60
R08E | 644 10 17 10 11 19 7 | 47 43 45 47 39 44
R09 | 1009 10 15 9 13 20 7 | 20 31 26 22 28 21
R11 | 491 19 13 11 20 17 9 | 19 29 27 38 23 26
R12 | 1440 21 12 20 11 29 9 | 24 29 38 26 33 25
R13 | 1292 25 33 32 28 24 17 | 44 39 31 35 29 34
R14 | 556 11 18 13 12 16 8 | 29 45 43 30 37 35
R15 | 556 19 11 21 16 18 10 | 36 38 46 28 28 34
R16 | 564 33 26 59 20 26 22 | 43 49 46 38 32 41
R17 | 513 10 14 13 12 12 7 | 49 37 36 49 45 42
R18 | 481 17 19 17 17 11 10 | 31 44 30 52 35 37
R19 | 1586 44 83 34 41 41 29 | 91 32 94 76 87 71
R20 | 2399 14 166 36 30 52 20 | 114 52 120 108 86 114
R21 | 440 9 23 11 10 17 7 | 65 47 63 65 71 61
XR22 | 1333 --- 355 9 7 18 8 | --- 123 40 34 31 35
R24 | 4499 12 32 10 11 21 9 | 63 43 57 59 45 55
------+------------------------------------+--------------------------------
RMS | 1501 20 48 24 18 24 |T 50 48 53 50 46 48
WRMS | 1501 19 30 15 15 19 |NE 48 45 49 47 43 45
MEDI | 917 13 18 13 12 18 |MD 44 43 45 47 39 42
Table 3.2247.4 GPS week: 2247 Day: 4 MJD: 59977
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 2122 28 55 39 23 32 20 | 49 60 54 44 43 41
R02E | 889 5 10 15 12 13 6 | 38 40 42 45 37 40
R03E | 1275 10 17 25 12 16 9 | 80 83 87 89 74 83
R04E | 1386 11 20 12 12 12 8 | 50 47 52 57 47 50
R05E | 1320 13 25 18 11 15 9 | 61 57 69 64 66 61
R07E | 944 9 18 12 8 10 6 | 58 47 58 58 56 55
R08E | 763 10 20 11 14 22 7 | 63 66 69 74 57 67
R09 | 685 12 13 17 13 22 8 | 23 30 28 24 26 23
R11 | 461 13 15 25 15 11 10 | 24 29 31 30 30 25
R12 | 1161 11 13 10 8 26 6 | 26 26 28 32 43 25
R13 | 715 16 59 45 55 31 25 | 35 34 39 43 42 32
R14 | 588 7 9 11 12 20 6 | 30 32 30 28 24 28
R15 | 678 9 15 14 10 24 7 | 29 40 30 41 24 33
R16 | 639 21 27 71 33 20 23 | 48 57 56 32 50 43
R17 | 604 15 16 10 12 11 8 | 53 40 44 43 45 45
R18 | 433 13 18 15 17 18 9 | 33 39 33 43 43 35
R19 | 3512 25 92 28 37 42 26 | 74 32 85 94 49 72
R20 | 1839 42 143 64 38 46 41 | 98 37 101 77 87 75
R21 | 551 6 23 21 13 28 9 | 58 47 70 55 77 57
XR22 | 1302 --- 392 13 10 26 11 | --- 122 44 41 34 40
R24 | 5466 23 27 19 16 16 12 | 71 56 54 55 52 58
------+------------------------------------+--------------------------------
RMS | 1764 17 45 29 22 24 |T 50 48 52 50 47 47
WRMS | 1764 16 35 23 16 19 |NE 46 44 48 45 44 42
MEDI | 889 12 20 17 13 20 |MD 49 40 52 44 45 43
Table 3.2247.5 GPS week: 2247 Day: 5 MJD: 59978
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 2011 33 45 27 20 28 18 | 49 47 55 41 43 41
R02E | 1010 12 18 15 9 13 7 | 30 35 30 36 24 30
R03E | 1761 12 15 12 16 25 8 | 119 120 119 122 106 119
R04E | 1614 11 16 16 12 17 8 | 46 44 46 55 39 46
R05E | 2145 9 14 13 10 18 6 | 55 55 56 58 61 55
R07E | 782 12 19 14 8 17 7 | 64 56 60 66 62 61
R08E | 986 15 20 13 14 15 9 | 66 73 66 72 61 68
R09 | 734 12 12 9 8 30 5 | 13 21 19 14 28 14
R11 | 631 10 14 17 9 19 7 | 17 24 19 20 23 17
R12 | 1049 10 12 21 9 13 7 | 20 25 30 25 21 21
R13 | 865 13 39 37 39 44 18 | 26 33 33 41 20 31
R14 | 1183 7 18 7 11 16 6 | 18 34 24 19 26 21
R15 | 1170 13 14 11 8 26 6 | 16 30 28 29 14 22
R16 | 886 23 25 62 17 20 20 | 30 44 28 33 34 30
R17 | 1244 16 15 14 18 11 9 | 40 41 42 33 31 36
R18 | 476 7 19 8 13 18 7 | 31 38 29 36 34 32
R19 | 1319 39 76 33 35 41 26 | 48 30 65 44 30 41
R20 | 1162 39 175 96 49 37 44 | 79 39 115 68 74 81
R21 | 1172 9 31 30 14 25 12 | 42 29 61 40 54 41
XR22 | 1590 --- 377 10 7 24 8 | --- 112 36 42 40 38
R24 | 2502 13 38 21 10 16 12 | 56 40 63 46 42 50
------+------------------------------------+--------------------------------
RMS | 1338 18 48 31 20 24 |T 43 46 48 44 41 42
WRMS | 1338 15 39 19 14 21 |NE 33 38 42 35 33 33
MEDI | 1170 12 19 15 12 19 |MD 40 39 42 41 34 38
Table 3.2247.6 GPS week: 2247 Day: 6 MJD: 59979
Weighted Average Orbit Dynamics (7 days)
PRN | brd cod esa gfz grg iac IGL | cod esa gfz grg iac IGL
------+------------------------------------+--------------------------------
R01E | 1806 33 49 69 61 20 31 | 40 48 85 62 41 40
R02E | 1379 9 15 10 12 17 6 | 60 60 59 67 59 61
R03E | 886 12 15 17 16 19 8 | 129 122 129 136 126 129
R04E | 1127 12 13 17 14 12 8 | 84 80 88 89 80 84
R05E | 2269 7 13 16 11 14 7 | 61 68 63 63 61 62
R07E | 604 9 23 14 11 29 8 | 73 66 67 68 62 68
R08E | 1168 14 21 22 21 30 11 | 96 87 97 109 84 98
R09 | 729 18 11 21 12 10 9 | 37 40 44 36 35 38
R11 | 718 6 13 10 8 15 5 | 34 39 43 40 37 37
R12 | 1149 18 10 12 14 12 8 | 32 33 41 31 39 32
R13 | 801 15 37 32 40 43 18 | 45 38 43 39 36 38
R14 | 1172 4 15 9 11 17 5 | 40 44 41 40 44 40
R15 | 758 15 14 17 9 15 8 | 38 41 47 42 36 39
R16 | 892 22 34 62 14 27 20 | 53 54 58 53 54 52
R17 | 1041 13 16 13 16 16 8 | 68 57 66 60 56 62
R18 | 773 17 11 16 12 18 8 | 48 65 63 66 55 58
R19 | 1724 31 55 22 41 41 22 | 85 31 80 89 57 71
R20 | 2052 69 138 66 49 47 47 | 120 57 133 105 110 104
R21 | 1717 10 28 10 13 14 9 | 82 64 86 84 85 79
XR22 | 1846 --- 370 13 11 26 12 | --- 173 43 41 42 39
R24 | 1470 20 31 19 13 18 12 | 88 58 81 76 67 76
------+------------------------------------+--------------------------------
RMS | 1300 22 40 30 25 24 |T 65 63 69 66 60 62
WRMS | 1300 16 30 23 19 22 |NE 59 56 62 57 53 54
MEDI | 1149 14 16 17 13 18 |MD 60 57 63 63 56 61
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